JPS6119954A - Rotary jet engine - Google Patents

Abstract

PURPOSE:To take out a strong rotational force to the outside with a simple structure, by utilizing a ram pressure and a pulse jet engine principle, injecting an explosion gas from an injection pipe to generate a strong propulsion force, and converting the propulsion force into a rotational force. CONSTITUTION:A rotational force is applied from the outside to a starting gear 22 to rotate a rotating center shaft 1. When engine speed is increased by the rotation, an air pushing effect is generated at an air intake opening 24 by a ram pressure to increase an air intake pressure. Then, the air is allowed to pass through injection pipes 5 and an exhaust shell 13, and is rearwardly exhausted. At this time, a valve plate alpha is opened by the ram pressure of the induction air. Under the condition, when fuel is injected from an injection nozzle 12, and is ignited by an ignition plug 23, an explosion power of the fuel is rearwardly transmitted through the injection pipes 5 and the exhaust shell 13 by a pulse jet engine effect, thereby generating a strong propulsion force. As a result, the rotating center shaft 1 is rotated through engine support rods 3 to provide a rotational force through an output gear meshed with a motive gear 19 to the outside of the engine.

Description

[Detailed description of the invention] The present invention relates to a rotary jet engine.

As is well known, conventional jet engines not only have a complex structure, but many of them were researched and developed for the purpose of making the aircraft equipped with the engine move in a straight line. It became possible to
Currently, no research or development has been conducted to extract the output of the Genod engine outside the aircraft and use it as a motive force for purposes other than aircraft movement. The present invention has been developed to solve these problems, and has developed a technology that uses a simple structure to transmit the large output of the Genod engine to the output phase outside the machine, convert it into rotational force, and use it as a variety of power sources. It was invented for the purpose of providing a rotary jet engine.

The present invention will be explained below based on the drawings. Reference numeral 1 indicates a rotation center axis provided in the vertical direction, and bearings 2.
Supported by 2. One end on the inside is fixed to the 3.3L rotation center axis l, and the other end is an engine support rod provided laterally on the left and right, respectively. This is a body part of a jet engine provided at one end of the outer side of each of the 4 and 41t engine support rods 3.3 in a direction substantially perpendicular to the support rods 3. Reference numerals 5, 5, . . . indicate injection tubes made of ceramic material and operated in a pulse genoad-like manner, which are provided in the body 4 of each jet engine in parallel with the engine support rod 3 at right angles. 6.6 is the body 4 of each jet engine
A ram pressure cylinder 6a is installed inside with an air suction network provided on one end side.
6a... are provided in a cylindrical shape. Reference numeral 7.7 denotes an air adjustment piece having a pointed cylindrical shape at the center of the inner diameter of the tip side of each air intake group 6. A is a bellows-shaped valve plate that is pivotally attached to the opening surface of each inner end surface of the ram pressure cylinder 6a so as to be opened and closed.

Reference numeral 8 denotes a fuel supply hole drilled inside the rotation center axis l parallel to the longitudinal direction of the rotation axis l, and one end thereof communicates with the fuel pressure pump 10 side via a /-rule 9 (e.g., a mechanical hole). However, the other end side is drilled up to the abbreviated length position of the entire length of the rotation center shaft 1. 1.11 connects one end of each to the fuel supply hole 8.
The other end is connected to the injection pipe 5 in the air intake group 6.
This is a fuel supply pipe that is bent and inserted in the front position. , 12.
12 is an injection nozzle attached to a portion inserted into the air intake assembly 6 at one end of the fuel supply pipe 11. 13.1
3 communicates the -4 side with the rear end side (the end opposite to the injection nozzle 12) of the body 4 of each jet engine, and the other end is bent downward to connect the downward exhaust hole 14. This is the cylindrical exhaust side provided. lε is the torso 4 of Ginotoe 7/n
It is a rotating bottom surface that is stretched horizontally in the form of a plate on the bottom side of the .

Reference numeral 16 denotes an exhaust surface provided in a bottomed cylindrical shape on the 1 side of the rotating bottom surface 15, and an outer circumferential side surface 17 is provided close to the outside of the outer circumferential portion of the rotating bottom surface 15. Reference numeral 18 denotes an exhaust pipe which has one end communicating with the bottom side of the exhaust surface 16 and the other end bent toward the outside of the machine. Reference numeral 19 is a driving gear wedged to the rotation center axis IK. 20 is an output side gear meshed with the driving gear 19. 2
1 is an output shaft inserted into the output side gear 20 and attached thereto. 22
is a starting gear meshed with the driving gear 19. Reference numeral 23 denotes an ignition punch provided at a position in front of the injection pipe 5. Since the great invention has such a structure, the operation will be described next. First, starting is performed by applying rotational force to the starting gear 22 from the outside, and when the driving gear 19 rotates, the rotation center shaft 1 rotates, and the rotation center shaft 1 rotates. ] The fuel supply pipe 11, which is fixed to the rotational center axis l by the rotation of the engine, the engine support rod 3, and the body part 4 of the engine and the rotating bottom surface 1, which are fixed to the tip thereof.
5 rotates as a unit. Therefore, when the aircraft speed increases due to this rotation, an air pushing effect occurs due to the ram pressure at the air intake port 24 on the tip side of the air intake network 6, and the air with increased inflow pressure passes through the injection pipe 5 and is exhausted. It is discharged rearward from side 13. At this time, the valve plate α is opened by the air inflow ram pressure. In this state, the fuel is pumped into the fuel supply hole 8 by the fuel pressure pump 10, injected from the injection nozzle 12 through the fuel supply pipe 1, and ignited by the ignition bushing 23, the explosive power of the fuel becomes pulsed. Due to the throat engine effect, it is ejected backward through each injection pipe 5, and further on the exhaust side 13.
A powerful propulsive force is generated as it ejects along the

At this time, the valve plate α is closed due to the slow rotational speed and low ram pressure during the initial explosion, but as the rotational speed increases due to the propulsive force, the ram pressure increases and the valve plate α remains open. In other words, it is open when the speed is high and air is passing through due to ram pressure, and when the explosion pressure is flowing toward the front in the opposite direction to the direction of the air flowing inside the shell and the propulsion force, it is closed and all the explosion pressure is effective. It has been improved so that it can be used as a propulsion force. As mentioned above, the valve plate a is strong because the ram pressure flowing inside the shell and the explosion pressure flowing counter-flow maintain a certain balance through rotation, so good results can be obtained even if it is not made of a sturdy valve. When a propulsive force is generated, the rotation center shaft 1 is rotated through the Enogino support rod 3.3, and this rotation rotates the output shaft 21 through the drive gear 19 and the output side gear 20 that meshes with it. It becomes possible to extract rotational force outside the machine. If the rotation continues in this state, ram pressure is constantly generated in the air intake port 24 and the ram FL cylinder 6a, and the explosion stroke is enabled by fuel injection, and the ram pressure engine 7 is generated in the front half of the horn. The second half of the engine/engine acts like a pulse generator engine, and together they operate as a generator engine based on a new principle. Moreover, in this case, even better results can be expected by giving the inside of the barrel a mirror finish. Therefore, the exhaust gas ejected from the exhaust network 13 is ejected from the exhaust hole 14 into the exhaust surface 16 below, and is further discharged to the outside of the machine from the exhaust pipe 18 provided below the exhaust surface 16.

When the present invention is implemented in this manner, the explosive gas is ejected from the ejection pipe using the ram pressure and the principle of a pulse no-nod engine, and is converted into rotational force (C structure f!i'). ], Q't ;(-1/A powerful rotation is announced:,
:tL°〉su1]-Q ′, 4 载J(+ (っSekibi, D'A ME・y], ノ1iJiヰ115...1′, ′ 1′f application No. 139513 The invention of the number is l+F] :',
During one rotation of a no-nod engine equipped with an injection pipe, the air intake side is directed in the direction of rotation so that the IJ axis rotates around the circumference of the CrVC. The main part of the present invention is a rotary no-throttle engine, which is attached to the left and right sides of the body, and transmits the propulsive force of the no-throttle engine to the rotational center shaft through an engine support rod and converts it into rotational force. The main part is that a jet engine equipped with a thin injection tube is mounted on the left and right with the air intake side facing the direction of rotation, so that the jet engine rotates circumferentially around the central axis of rotation, and the central axis of rotation is rotated. However, the difference is that a ram pressure cylinder with an opening/closing piece is provided in the front half of the body of the no-nod engine, and the purpose is to use the same rotary no-nod engine as the rotary-type Jeep R of the original patent invention. This invention achieves the same purpose as the original patented invention.

[Brief explanation of drawings]

FIG. 1 is a front view of the present invention. FIG. 2 is a plan view. 1...Rotation center shaft 2...Bearing 3rd piece
Engine support rod 48. , jet engine
Body part 5...Injection pipe 6...Air suction side 6a.
... Ram pressure cylinder a... Valve plate 7... Air adjustment piece 8... Fuel supply hole 91.・/ -le 10...Fuel pressure pump 11...Fuel supply pipe 12...Injection nozzle 13...Exhaust network
]4...Exhaust hole 15--1 rotation bottom J6...
・Exhaust Box Figure 2 Procedural Amendment (Method) % Formula % 1 Case Indication 1981 Patent Application No. 141134
No. 2 Name of the invention Rotary jet engine 3, person making the amendment Relationship to the Takashi Uesugi case
Patent Applicant 4, Agent 3-4-27 Shimosawa-dori, Hyogo-ku, Kobe, Japan Date of amendment order: October 9, 1980 (Delivery date: October 30, 1980) 6. Amendment subject to amendment On page 1, line 16 of the official specification, it is stated that ``q The present invention relates to a rotary jet engine.・
``...'' it says. 3. Detailed Description of the Invention The present invention relates to a rotary jet engine. ``...'' I corrected myself. Procedural amendment dated February 7, 1985 1, case description 1981 patent application No. 141134
No. 2, Title of the invention Rotary jet engine 3, Name to be amended Relationship to the Takashi Uesugi case Patent applicant 5, Date of amendment order Voluntary amendment

Claims (1)

[Claims] (1) A jet engine is equipped with a thin injection pipe in the rear half of the body, and a ram pressure cylinder and a valve plate for opening and closing the ram pressure cylinder in the front half, with the jet engine centered around the central axis of rotation. In order to rotate around the circumference, the jet engine is installed on the left and right with the air intake side facing the direction of rotation, and an ignition device is installed in the center of the body, and the propulsive force of the jet engine generated by ignition is transmitted to the rotation center shaft by the engine support rod. A rotary jet engine that converts the energy into rotational force.